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General guidelines for inspection and maintenance of control surfaces.
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Corrosion and pitting on control cable attachment fittings could lead to loss of some flight controls.
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Over time, a chafing condition resulting from the control cable sliding against the stationary pulley groove can cause the control cable to wear completely through, possibly resulting in loss of aileron control during flight.
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Installing newly designed tail brace wire nipples to avoid fatigue failures.
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Reports of the end fittings on the tailwheel shock cords pulling off during taxi procedures. Includes repair procedures.
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Provides inspection and fatigue life requirements applicable to the wing lift strut forks.
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The use of automotive type gasoline in General Aviation aircraft is believed to be a contributing factor in numerous accident investigation reports.
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Recommended inspection of the sealing of firewall holes.
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Refinishing procedure for airplanes which are finished with Nitrate dope and which are to be refinished with Butyrate dope, or "Duraclad".
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Safety procedure instructions which must become an integral part of the aircraft owner's operational routine and/or preflight inspection.